SAE ARP4028-1994
Aircraft/Engine Fuel Pump Two Phase (Slugging Flow) Inlet Performance Test and Evaluation

Standard No.
SAE ARP4028-1994
Release Date
1994
Published By
Society of Automotive Engineers (SAE)
Status
Replace By
SAE ARP4028-2020
Latest
SAE ARP4028-2020
Scope
This procedure is intended to apply to all engine or airframe mounted fuel pumps and controls when required by the applicable specification. The procedure recommends a recirculation system similar to ARP492 to control the fuel properties affecting the fluid and its ability to "release" fuel vapors and dissolved air and have these "re-entrained or dissolved" during the fluid recovery process back to the tank and the original starting conditions. This SAE Aerospace Recommended Practice (ARP) defines procedures for testing aircraft/engine fuel pumps for the purpose of: a. determining two phase ("slugging flow") inlet performance capability; b. determining the pump's resistance to deterioration during an endurance test with the operating conditions defined by the applicable specification which includes two phase ("slugging flow") operation; and c. determining the effects that contaminated fuel operation may have had on two phase ("slugging flow") inlet performance. The procedure recommended herein is intended to produce useful, reproducible, steady state results. This test is not intended to establish maximum starting altitude or rate of climb performance of the pump. This procedure defines recommended test setups, test procedures, and data requirements for testing engine or airframe mounted fuel pumps or controls with pumps for the purpose of determining "slugging flow" inlet performance capability

SAE ARP4028-1994 Referenced Document

  • ASTM D323-94 Standard Test Method for Vapor Pressure of Petroleum Products (Reid Method)
  • ASTM D86-93 Standard Test Method for Distillation of Petroleum Products
  • SAE AIR1326-1974 Aircraft Fuel System Vapor-Liquid Ratio Parameter
  • SAE ARP492 AIRCRAFT FUEL PUMP CAVITATION ENDURANCE TEST
  • SAE MAP749B-1992 AIRCRAFT TURBINE ENGINE FUEL SYSTEM COMPONENT ENDURANCE TEST PROCEDURE (ROOM TEMPERATURE CONTAMINATED FUEL)

SAE ARP4028-1994 history

  • 2020 SAE ARP4028-2020 Aircraft/Engine Fuel Pump Two Phase (Slugging Flow) Inlet Performance Test and Evaluation
  • 1994 SAE ARP4028-1994 Aircraft/Engine Fuel Pump Two Phase (Slugging Flow) Inlet Performance Test and Evaluation



Copyright ©2024 All Rights Reserved